Statements (29)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
piston engine
|
| gptkbp:configuration |
axial-flow
|
| gptkbp:countryOfOrigin |
gptkb:United_Kingdom
|
| gptkbp:developedBy |
gptkb:Bristol_Theseus
|
| gptkbp:diameter |
3 ft 10 in (1.17 m)
|
| gptkbp:enteredService |
1952
|
| gptkbp:firstFlight |
1947
|
| gptkbp:fuelType |
kerosene
|
| https://www.w3.org/2000/01/rdf-schema#label |
Bristol Proteus
|
| gptkbp:length |
12 ft 2 in (3.71 m)
|
| gptkbp:manufacturer |
gptkb:Bristol_Aeroplane_Company
|
| gptkbp:notableFeature |
contra-rotating propellers (in some variants)
reverse-flow combustion chambers |
| gptkbp:numberOfStages |
2
12 |
| gptkbp:powerOutput |
3,780–4,450 shp
|
| gptkbp:retired |
1980s
|
| gptkbp:successor |
gptkb:Rolls-Royce_Tyne
|
| gptkbp:type |
free-turbine turboprop
|
| gptkbp:usedIn |
gptkb:SR.N4_hovercraft
marine applications |
| gptkbp:usedInAircraft |
gptkb:Fairey_Rotodyne
gptkb:Bristol_Britannia gptkb:Blackburn_Beverley gptkb:Saunders-Roe_Princess |
| gptkbp:weight |
2,800 lb (1,270 kg)
|
| gptkbp:bfsParent |
gptkb:Bristol_Centaurus
gptkb:Bristol_Britannia |
| gptkbp:bfsLayer |
6
|